All,
The apogee contact had a low receive AGC, so only minimal commanding was performed. The Orbit 660 ATS was not uplinked. This will be completed during the upcoming perigee contacts. The Inertial maneuver was successful.
Results from the Inertial Maneuver:
Q1 0.53523800 ActNor.EstInrToBdy[0]
Q2 -0.33831000 ActNor.EstInrToBdy[1]
Q3 -0.77096100 ActNor.EstInrToBdy[2]
Q4 0.06845670 ActNor.EstInrToBdy[3]
GPS sec 1408663930 ActNor.EstTime
UTC time 08/25/2024 23:31:56 output
MPS Cmd Vector X -0.87362800
MPS Cmd Vector Y 0.45021800
MPS Cmd Vector Z 0.18460300
CSS Angle TLM 0.723887
CSS Sun-Pointing Angle 1.447774
21 Aug 24 @12:00:00
CSS Angle TLM 0.349246
CSS Sun-Pointing Angle 0.698492
25 Aug 24 @23:30:00
Pre-Burn
Thruster 1 4368 21 Aug 24 @12:00:00
Thruster 2 4304
Thruster 3 4608
Thruster 4 4672
Post-Burn
Thruster 1 4672 25 Aug 24 @23:30:00
Thruster 2 4576
Thruster 3 4880
Thruster 4 4976
Number of Pulses
Thruster 1 304
Thruster 2 272
Thruster 3 272
Thruster 4 304
Thruster Pairs
Thruster 1 & 2 576
Thruster 3 & 4 576
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
IBEX MOC (703)404-7470
Cell (301) 606-1430